| AE3007A3 ✕ | |
|---|---|
| EASA ID | 01P06AL034 |
| Aircraft Engine Manufacturer | Rolls-Royce |
| Aircraft Engine Type | Turbofan |
| Fuel | Jet A |
| Geared Fan | No |
| Combustion Chamber | Type 3 (reduced emissions) |
| Afterburner | No |
| Streams | 2 |
| Bypass Ratio | 4.72 |
| Overall Pressure Ratio | 17.2 |
| Maximum Takeoff Thrust (kN) | 33 |
| Hydrocarbon Take Off (g/kg fuel) | 0.03 |
| Hydrocarbon Climb Out (g/kg fuel) | 0.03 |
| Hydrocarbon Approach (g/kg fuel) | 0.03 |
| Hydrocarbon Idle (g/kg fuel) | 4.1 |
| Hydrocarbon Unitary Average (g/kN) | 8.75 |
| Hydrocarbon Unitary Characteristic (g/kN) | 13.48 |
| Hydrocarbon Unitary Characteristicto Regulatory (% of limit) | 68.8 |
| Hydrocarbon LTO (g) | 289 |
| Carbon Monoxide Take Off (g/kg fuel) | 0.5 |
| Carbon Monoxide Climb Out (g/kg fuel) | 0.5 |
| Carbon Monoxide Approach (g/kg fuel) | 7.65 |
| Carbon Monoxide Idle (g/kg fuel) | 41.29 |
| Carbon Monoxide Unitary Average (g/kN) | 94.25 |
| Carbon Monoxide Unitary Characteristic (g/kN) | 115.69 |
| Carbon Monoxide Unitary Characteristicto Regulatory (% of limit) | 98 |
| NOx Take Off (g/kg fuel) | 15.4 |
| NOx Climb Out (g/kg fuel) | 13.48 |
| NOx Approach (g/kg fuel) | 6.93 |
| NOx Idle (g/kg fuel) | 4.12 |
| NOx Unitary Average (g/kN) | 37.32 |
| NOx Unitary Characteristic (g/kN) | 43.26 |
| NOx Unitaryto Standard (% of limit) | 58.1 |
| NOx Unitaryto CAEP2 (% of limit) | 72.7 |
| NOx Unitaryto CAEP4 (% of limit) | 74.3 |
| NOx Unitaryto CAEP6 (% of limit) | 75.1 |
| NOx Unitaryto CAEP8 (% of limit) | 80 |
| NOx LTO (g) | 1232 |
| Smoke Take Off (SN) | 0.01 |
| Smoke Climb Out (SN) | 0.01 |
| Smoke Approach (SN) | 0.01 |
| Smoke Idle (SN) | 0.01 |
| Smoke Max (SN) | 0.01 |
| Smoke Characteristic (SN) | 0.01 |
| Smoke Characteristicto Regulatory (% of limit) | 0 |
| Fuel Flow Take Off (kg/s) | 0.3583 |
| Fuel Flow Climbout (kg/s) | 0.2995 |
| Fuel Flow Approach (kg/s) | 0.1076 |
| Fuel Flow Idle (kg/s) | 0.0448 |
| Fuel LTO (kg) | 150 |
| Carbon Monoxide LTO (g) | 3111 |
| Emissions Data Status | C |
| Engine Status | Out of production |
| NOx Compliance Demonstration | 2.3.2 e) |
| nvPME Imass Approach (mg/kg) | 9.9862 |
| nvPME Imass Climb Out (mg/kg) | 32.8059 |
| nvPME Imass Idle (mg/kg) | 18.7923 |
| nvPME Imass Max (mg/kg) | 41.3455 |
| nvPME Imass Take Off (mg/kg) | 41.3455 |
| nvPME Inum Approach (#/kg) | 332255800000000 |
| nvPME Inum Climb Out (#/kg) | 312347000000000 |
| nvPME Inum Idle (#/kg) | 658652900000000 |
| nvPME Inum Max (#/kg) | 658652900000000 |
| nvPME Inum Take Off (#/kg) | 293709900000000 |
| nvPMLTO Mass (mg) | 3696.384 |
| nvPMLTO Mass Per Thrust (mg/kN) | 153.1 |
| nvPMLTO Mass To CAEP11 (% of limit) | 15 |
| nvPMLTO Number (#) | 76873510000000000 |
| nvPMLTO Number Per Thrust (#/kN) | 3180000000000000 |
| nvPMLTO Number To CAEP11 (% of limit) | 26.1 |
| nvPM Mass Concentration Characteristic (mg/m³) | 242 |
| nvPM Mass Concentration Max (mg/m³) | 188.3518 |
| nvPM Mass Concentration To CAEP10 (% of limit) | 1.9 |